Accession Number:

ADA070192

Title:

A Force and Moment Test of a 1/24-Scale F-111 Model at Mach Numbers from 0.7 to 1.3.

Descriptive Note:

Final rept.,

Corporate Author:

ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFS TN

Personal Author(s):

Report Date:

1979-03-02

Pagination or Media Count:

16.0

Abstract:

A test program was conducted in the Propulsion Wind Tunnel 16T to determine forces and moments on a 124-scale F-111 model. Data were obtained at Mach numbers from 0.7 to 1.3 at total pressures of 1200 and 2000 psfa. Model angle of attack was varied from -2 to 20 deg at 0-deg sideslip. Sideslip angles were varied from -10 to 10 deg at 10- and 15-deg angles of attack. Author

Subject Categories:

  • Aerodynamics
  • Attack and Fighter Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE